机电设备2024,Vol.41Issue(1) :10-15.DOI:10.16443/j.cnki.31-1420.2024.01.003

减摇陀螺飞轮动力学特性分析

Dynamic Characteristic Analysis of Ship Gyro-Stabilizer Flywheel

杜一帆 刘少卿 王文杰 周健
机电设备2024,Vol.41Issue(1) :10-15.DOI:10.16443/j.cnki.31-1420.2024.01.003

减摇陀螺飞轮动力学特性分析

Dynamic Characteristic Analysis of Ship Gyro-Stabilizer Flywheel

杜一帆 1刘少卿 2王文杰 1周健1
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作者信息

  • 1. 上海衡拓船舶设备有限公司,上海 200031
  • 2. 上海船舶设备研究所,上海 200031
  • 折叠

摘要

以某型减摇陀螺装置飞轮为研究对象,采用ANSYS Workbench建立有限元模型,对飞轮进行模态分析,计算飞轮自身的临界转速并绘制坎贝尔图;结合飞轮本身的不平衡量,通过谐响应分析方法得到飞轮的稳态不平衡响应曲线.结果显示:飞轮的1阶临界转速为8 732.5 r/min,工作转速低于1阶临界转速的70%,不会产生共振;在不平衡量的作用下,飞轮在202 Hz、218 Hz下会产生明显的共振现象,该频率远高于飞轮的工作转速,因此在飞轮正常工作时不会受到飞轮不平衡量引起的共振.证明该型减摇陀螺装置飞轮设计的合理性,同时对后续同类型飞轮的设计提供仿真参考.

Abstract

Taking the flywheel of a type of ship gyro-stabilizer as the research object,establish finite element model with ANSYS Workbench to launch the modal analysis of the flywheel,and calculate the critical speed of the flywheel and the Campbell diagram is drawn.Then combined with the unbalance of the flywheel itself,the steady-state unbalance response curve of the flywheel is obtained by harmonic response analysis method.The results show that the first critical speed of the flywheel is 8 732.5 r/min,and the working speed is lower than 70%of the first critical speed,so there is no resonance.Under the action of the unbalance,the flywheel will have obvious resonance at 202 Hz and 218 Hz.This frequency is far higher than the working speed of the flywheel,so the flywheel will not be subject to the resonance caused by the flywheel unbalance during normal operation.The rationality of the flywheel design of this type of anti rolling gyro device is proved,and the simulation reference for the subsequent design of the same type of flywheel is provided.

关键词

减摇陀螺/飞轮/模态分析/谐响应分析

Key words

gyro-stabilizer/flywheel/modal analysis/harmonic response analysis

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出版年

2024
机电设备
上海船舶设备研究所

机电设备

影响因子:0.125
ISSN:1005-8354
参考文献量7
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